JASC 2910
Service difficulty reports · 11,292
Reports filed under 2910 · Hydraulic System, Main, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2910' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2910' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA000501006Valve · failed(CAN) NR 2 HYD PUMP FAILED. INVESTIGATION REVEALED A LEAKING ISOLATION VALVE.SDR USAASB00119Tube · crackedBWI - FLT 988 - UPON LIFTOFF, JUST AFTER GEAR RETRACTION, CAPTAIN RECEIVED INDICATION OF SYSTEM A HYDRAULIC LOSS. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND SHUTDOWN BOTH SYSTEM A PUMPS WITHIN TWO MINUTES. FLIGHT DIVERTED TO BWI AND LANDED WITSDR HALA0000131Valve · leakingFLT 932 - HNL - AIR RETURN, ON CLIMB-OUT, NR 2 HYD LEAK, (2 GAL REMAINING). REMOVED AND REPLACED 2-1 NON-REVERSIBLE PUMP SHUTOFF VALVE PER MM 27-26-03. OPS/LEAK CHECK OK. SERVICED HYD QTY. (M)SDR DL757000767B-Nut · looseAFTER T/O CABIN AND FLIGHT CREW SMELLED BURNING ELECTRIC ACRID ODOR. PAX COMPLAINED OF BURNING EYES. RETURNED TO CVG. FOUND HYD LEAK IN RIGHT W/W. TIGHTEN B- NUT ON LINE FROM HYD FILTER RETURN LINE.SDR DLL10000757Elbow · crackedSYSTEM B HYDRAULIC RESEVIOR LEVEL DECREASED TO .25. TANK SHUT DOWN SYSTEM. REPLACED ELBOW ON PRESSURE LINE ON NR 2 ENGINE, HYD PUMP AND REPLACED PACKING ON TRANSFER LINE ON LEFT ELEVATOR FEEL UNIT. PERFORMED LEAK CHECK, NO DISCREPANCIES ENCOUNTERED.SDR CA000427008Line · leaking(CAN) SHORTLY AFTER DEPARTURE CREW ADVISED THAT FLIGHT CONTROL HYD SYS HAD DEPLETED AND THE ASSOCIATED PUMPS OFF LOADED.. SUPPLY LINE FROM THE FLIGHT CONTROL PUMP IN THE NR 2 STUB WING HAD FAILED. LINE REPLACED AC SERICEABLE.SDR DL72S000719Sequence Valve · chafedAFTER T/O LOST A SYS HYD FLUID. AIR TURNBACK TO ABQ. FOUND LINE IN RT MAIN GEAR FROM SEQUENCE VALVE CHAFED THROUGH. MTC REPLACING SAME.SDR AU000444Pipe · cracked(AUS) RIGHT HYDRAULIC FILTER PRESSURE PIPE SPLIT AND LEAKING AT OUTBOARD RADIUS. LOSS OF HYDRAULIC FLUID.SDR CA000427006O-Ring · leaking(CAN) CREW REPORTED THAT THE NR 1 HYD SYS QTY WAS DROPPING SLOWLY. QTY FINALLY DROPPED INTO YELLOW AND AC DIVERTED. LEAK IN NR 2 WING STUB AT SILENCER. LINE REMOVED AND INSPECTED, NO CRACKS, NEW SEAL INSTALLED, AC SERVICEABLE.SDR USAASB00113Line · chafedCLT - FLT 825 - ON DESCENT INTO CLT, CAPTAIN REPOTED THE NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. CAPTAIN POSITIONED THE NR 1 ENGINE HYDRAULIC SWITCH TO OFF AND DECLARED AN EMEGENCY. FLIGHT LANDED WITHOUT FURTEHR INCIDENT. AIRCRAFT WAS TOWED TOSDR UPS00232307Line · burstINSPECTION TYPE:C, PRESSURE LINE IN B SYS HYD SERVICE BAY BURST ON OPERATION. FAILED UNDER P-CLIP AREA. PRESSURE LINE IN B-SYS HYD SERVICE BAY REPLACED IAW MM 20-80-01. LEAK CHECKED OK.SDR CA000414008Tube · chafed(CAN) NO 2 SYS A LOW PRESS WARNING LIGHT ON IN FLIGHT WITH A LOSS OF SYS QTY ON APPROACH. NO 1 A SYS LOW PRESS WARNING LIGHT ON RESULTING IN LOSS OF SYS HYD. CHAFED HYD LINE ABOVE RH MLG ACTUATOR. LINE REPLACED. AC SERVICEABLE.SDR HALA0000114Shutoff Valve · leakingHNL - FLT 6 - HYD SYSTEM 3 ELEV OFF LIGHT CAME ON DURING CLIMB-OUT. A/C DIVERTED TO HNL, WHERE AN UNEVENTFUL LANDING WAS MADE. FOUND 3-2 NON REVERSIBLE SHUTOFF VALVE LEAKING. REMOVED AND REPLACED SHUTOFF VALVE. RESERVICED HYD RES BLED SYSTEM. SHUT OFF VALSDR CA000410001Tube · failed(CAN) LEAK OUTSIDE LEFT NACELLE - MIX OF HYDRAULIC FLUID AND OIL. LIFT DUMP PRESSURE TUBE REPLACED AND A/C RETURNED TO SERVICE.SDR DL72W000645Line · brokenFIFTEEN MINUTES OUT OF DCA, FLIGHT CREW REPORTED A HYDRAULIC SYSTEM FLUID LOSS. FOUND HYDRAULIC LINE LEAKING. REPLACED SAME.SDR SWIA971754Valve · failedBLUE SYSTEM LOW PRESS LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO PDX. REPLACED MOISTURE PURGE VALVE IAW MM 29-14-00, OPS CHECK GOOD.SDR DL72S000637Line · chafedA SYSTEM FAILURE. FOUND LINE TO NR 2 LEAKING. REPLACED WITH TEMP/APPROVED LINE. LEAK AND OPS CKS GOOD. HYD FLUID AT 3 GAL.SDR AWXA0000221Filter · cloggedAIR TURNBACK, FLT CONTROL WARNING. ON CLIMBOUT FROM PHX, MASTER CAUTION LIGHT AND FLIGHT CONTROL ANNUNCIATOR ILLUMINATED FEEL DIFF PRESS, WHEN MASTER CAUTION WAS RESET FEEL DIFF PRESS REMAINED ON. REMOVED AND REPLACED A AND B SYS HYD RETURN FILTERS (NO VISUASDR UPS00232190Line · crackedAIR TURN BACK ON DELIVERY FLIGHT FROM C CHECK AT SNN . CREW EXPERIENCED TOTAL LOSS OF B SYSTEM HYD PRESS . PRESS LINE FROM NR 1 B PUMP TO B SYS PRESS MODULE FOUND FRACTURED AT SLEEVE PRESS LINE CANIBALIZED FROM A/C N912UP TO REPLACE FRACTURED PIPE LINE. HYD SSDR DL76L000619Line · leakingLEFT HYD QTY LEAK DURING CRUISE, RIGHT DISENGAGED AND CENTER A/P OK. FOUND LEAKING HYD RETURN LINE IN LEFT PYLON. REPLACED SAME WITH AA PURCHASED PART. PRESSURIZED HYD, NO LEAKS. RAN FCC RIGHT TEST, NO FAULTS. OK FOR SERVICE. SDR 00FDEA00364Hydraulic System · leakingAFT LEVEL OFF FL310 HYD NR 2 QTY DOWN TO 5.0 GAL. QTY WENT LOWER TO 2.7 GAL. PUMPS AUTO SHUTDOWN. DIVERT TO TPE. *S/D* REMOVED HYD TUB AND FAB TUB BY CHINA AIRLINES AND INSTALLED. REMOVED AND REPLACED HYD ENG MANIFOLD AND SYS MANIFOLD FILTER ELEMENTS PERSDR RRXA000197Line · rupturedHYD FLUID MAIN RES LOSS TO AUX LEVEL; USED AUX PUMP FOR NORM SYSTEM OPS. AFTER BY-PASS MAIN SYS & PUMPS. DISCOVERED RT ENG DRIVEN HYD PUMP MAIN PRESSURE SUPPLY LINE RUPTURED FABRICATED AND INSTALLED LIKE HYDRAULIC LINE ASSY. RESECURED HYD RESERVOIR, LK CK SDR JBXA0000162Filter · cloggedAT FL 350 HYD SYS 1 OVERHEAT FAULT LIGHT ILLUMINATED. RETURNED TO RDU. REMOVED AND REPLACED NR 1 HYDRAULIC SYSTEM RETURN FILTER IAW AMM 29-13-05 AND NR 1 ENGINE SYSTEM 1 AND 2 PUMPS IAW AMM 29-11-01 AND NR 2 ENGINE SYSTEM 1 HYD PUMP IAW AMM 29-11-01. PERFORSDR 20000510SH028Line · looseRIGHT ENGINE NR 2 SYSTEM HYDRAULIC PRESSURE LINE BECAME UN-SWAGED AT OUTBOARD END CAUSING COMPLETE DRAINAGE OF NR 1 HYDRAULIC SYSTEM. THIS OCCURRED IN-FLIGHT. FURTHER INVESTIGATION REVEALED IMPROPER SWAGING. TUBE WAS INSTALLED APPROXIMATELY 1 WEEK PRIOR TO ISDR 00FDEA00196Warning Light · illuminatedA-SYS HYD QUANTITY DROP TO ZERO FOLLOWED BY NR 1 LOW PRESSURE LIGHT ILLUM. REMOVED AND REPLACED O-RING PER MM 29-11-000-1.SDR CA000331002Line · failed(CAN) HYDRAULIC PRESSURE LINE TO LIFT DUMP VALVE FOUND LEAKING AT SWAGED FITTING. LINE REPLACED.SDR AALA20000050Line · leakingPLS - FLT 625 - DURING DESCENT INTO PLS, SYSTEM 'B' HYDRAULIC FAILURE. CREW DECLARED EMERGENCY AND LANDED PLS WITHOUT INCIDENT. REPLACED PRESSURE LINE ON NR 2 PUMP. SYSTEM GROUND CHECK NORMAL OPERATION. REPLACED WITH TEMPORARY HOSE. (M)SDR TWAA0005002Line · leakingTHE CREW REPORTED BRAKES DRAGGING AS AIRCRAFT WAS TAXIED INTO THE GATE. AFTER BRAKES WERE PARKED A FIRE IGNITED AT THE NUMBER 2 FRONT BRAKE AND TIRE ASSEMBLY. THE FIRE WAS QUICKLY EXTINGUISHED, IT WAS CAUSED BY HYDRAULIC FLUID LEAKING DOWN ONTO THE WHEEL ANDSDR EISA2000040Drive Gear · leakingFOUND LOSS OF A SYSTEM HYDRAULIC POWER. EMERGENCY DECLARED LANDING OK. TAXI OK. TOWED TO BLOCKS. FOUND OUTBOARD FLAP HYDRAULIC DRIVE MOTOR LEAKING. REMOVED AND REPLACED TRAILING EDGE FLAP DRIVE MOTOR. LEAK AND OPERATIONAL CHECK GOOD. (M)SDR PLGA000325Line · rupturedBGR - FLT 4601 - AFTER TAKEOFF FROM BGR, CREW SELECTED GEAR UP AND GOT AN IMMEDIATE HYDRAULIC FAILURE LIGHT ON THE CWP FOLLOWED BY HYDRAULIC QUANTITY DROPPING TO ZERO. CREW DIVERTED BACK TO BGR AND LANDED WITHOUT INCIDENT. AFTER LANDING AND STOPPING, THE CRESDR 2000UALA00153Line · leakingLOST OF SYSTEM ''A'' HYDRAULICS DUE TO A HYDRAULIC LEAK FROM A FLEX LINE. *S/D* LEAK WAS FOUND COMING FROM LEFT HAND MAIN LANDING GEAR LOCK ACTUATOR. REPLACED DAMAGED HYDRAULIC FLEX LINE.SDR 20000522AP001Valve · failedUPON REACHING CRUISE ALT FL310, AIRCRAFT EXPERIENCED TOTAL SYSTEM A HYD FAILURE. ACCOMPLISHED ''A'' SYSTEM HYDRAULIC FAILURE CHECKLIST, IAW AOM VOL 1 EMERGENCY PROCEDURES. DECLARED AN EMERGENCY AND RETURNED TO MIAMI, DID NOT DUMP FUEL. FOUND 3 WAY VALVE IN SDR CA000331001Line · failed(CAN) HYDRAULIC SUPPLY LINE TO PRESSURE MANIFOLD LEAKING. HYDRAULIC TUBE REPLACED.SDR QXEA0000968Line · chafedPDX - LEFT-HAND HYDRAULIC FLEX LINES CHAFING ON STRUCTURE AFT OF SHUT-OFF VALVE. REPAIRED IAW FOKKER SRM 55-31-01, PAGE 4, FIGURE 1, ITEM 890 AND SRM 51-31-01.SDR 0001019997Line · leakingAFTER SLAT RETRACTION, THE RIGHT HYDRAULIC SYSTEM DROPPED TO ZERO QUANTITY AND PRESSURE. CREW DECLARED A YELLOW EMERGENCY AND FLIGHT WAS RETURNED TO MCI. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE LEAKING AT LEFT WING FORWARD SPAR. SDR JBXA0000157Swivel · leakingON PRE-FLIGHT, CREW FOUND HYD FLUID LEAKING ON NOSE WHEEL AREA. MX INSPECTED AND FOUND NLG SWIVEL LEAKING.SDR CA000329027Line · leaking(CAN) DURING ROUTINE OVERNIGHT, HYDRAULIC FLUID WAS FOUND SEEPING FROM THE RIGHT MLG REAR AND CENTER DOOR ACTUATOR EXTEND FLEX LINE. TEMPORARY LINE INSTALLED.SDR AU000337Pipe · cracked(AUS) HYDRAULIC PIPE LOCATED IN LH WHEEL WELL CRACKED AND LEAKING.SDR CA000329026Line · leaking(CAN) AFTER ARRIVAL, HYDRAULIC FLUID WAS FOUND LEAKING FROM 32 NACELLE. INVESTIGATORS REVEALED THAT BOTH UP AND DOWN LINE FOR THE RT MAIN GEAR ACTUATOR WERE LEAKING. LINES REPLACED.SDR 20000501SH009Hose · deterioratedSTRATOFLEX HOSE NR 111-4, CURE DATE 3Q92, FULLY DETERIORATED WHILE INSTALLED ON BELGIAN REGISTERED AIRCRAFT. NO OTHER CASES FOUND WITH INSTALLED HOSES. THIS PART WAS BOUGHT THROUGH GILL AVIATION, VIA AVIALL. HOSE INSTALLED ON A ROCKWELL 112, WITH LYC IO-360SDR P2EA00067Hydraulic Line · leakingPIT - FLT 701 - AIR RETURN TO PIT, EMERGENCY DECLARED, LANDING UNEVENTFUL. LOST A SYSTEM HYDRAULIC QUANTITY AND PRESSURE IN FLIGHT. REPLACED RIGHT WING SPOILER SYSTEM HYDRAULIC RETURN LINE WITH TEMPORARY FLEX LINE. SERVICED A HYDRAULIC SYSTEM PER MM 12-12-0SDR DHL2000727002Hydraulic System · lowEN ROUTE FROM SJU TO CVG, NOTICED A LOW A-SYSTEM QUANTITY AND FLUCTUATING HYDRAULIC PRESSURE. FLIGHT WAS DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. SERVICED TO FULL 1.3 GALLONS, RAN NR 1 AND NR 2 ENGINES AND FLAPS UP AND DOWN. CYCLED SPEED BRAKES AND SPOSDR 0000875507Hose · failedDURING CLIMB AFTER DEPARTING FROM DTW, LOST LEFT HYDRAULIC SYSTEM PRESSURE AND LEFT HYDRAULIC QUANTITY. PERFORMED ALTERNATE GEAR AND FLAPS EXTENSION. RETURNED FOR AN UNEVENTFUL LANDING IN DTW. MAINTENANCE REPLACED BURST FLEX HOSE IN NOSE GEAR WELL, SERVICEDSDR TSAA0029077Hydraulic Line · brokenFLT 86 - HNL-KOA - DURING TAKEOFF, EXPERIENCED A COMPLETE LOSS OF A SYSTEM HYDRAULICS. PERFORMED CHECKSLIST AND RETURNED TO HNL FOR AN UNEVENTFUL LANDING. AFTER LANDIG THE STANDBY LOW QUANTITY LIGHT CAME ON. AFTER THE LANDING GEAR WAS LOWERED, WAS UNABLE TOSDR 20000424AP002Packing · damagedMIA - FLT TA823 - DURNG TAKEOFF, THE AIRCRAFT LOST ALL OF BLUE HYDRAULIC SYSTEM FLUID. THE AIRCRAFT RETURNED TO MIA AIRPORT FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING, MAINTENANCE TECHS FOUND THE BLUE SYSTEM HYDRAULIC PRESSURE SWITCH PACKING DAMAGED. THE SDR CA001106009Line · fractured(CAN) CLIMBING THOUGH FL80 FROM COPENHAGEN, 1ST OFFICER REPORTED LOSS OF NR 2 HYDRAULIC SYSTEM CONTENTS. AIRCRAFT RETURNED TO COPENHAGEN, CARRYING OUT ACTION IAW EMERGENCY CHECKLIST NR 2 HYDRAULIC SYSTEM FLUID LOSS. AIRCRAFT STATICS: TOTAL HOURS 4532.10 TOTSDR AU000187Filter · leaking(AUS) LT HYDRAULIC SYSTEM NR 2 PRESSURE LINE FILTER LEAKING BETWEEN THEHEAD AND HOUSING DUE TO LOOSE BACKUP O-RING SEAL.SDR 0000882297Line · failedIN CRUISE FLIGHT, THE 'B' SYSTEM LOW PRESSURE LIGHT ILLUMINATED FOLLOWED BY PRESSURE FLUCTUATIONS. 'B' SYSTEM QUANTITY DROPPED TO ZERO. CREW PERFORMED COM PROCEDURE AND LANDED WITHOUT INCIDENT. DTW MAINTENANCE REPLACED DEFECTIVE FLEX LINE RUNNING FROM RESERSDR CA000315006Packing · deteriorated(CAN) DURING CLIMB LT ENG HYD QTY DECREASED BY 20 PERCENT, CREW TURNED OFF LT HYD SYS HYD PUMP AND LANDED STFELY. REPLACED PACKING AND TEST SERV. DURING DEICING NR 1 HYD PUMP FAILED. REPLACED, PLUS CASE AND RETURN FILTERS REPLACED.SDR CA000315004Line · leaking(CAN) ON START-UP, THE GROUND HANDLER NOTICED HYDRAULIC FLUID DRIPPING FROM THE NOSE GEAR AREA. INVESTIGATION REVEALED THAT THERE WAS A PIN HOLE IN THE NLG UP LINE FWD OF OXYGEN BOTTLES.
Back to JASC 2910